Blade seal for an aircraft

Aeronautics and astronautics – Aircraft sustentation – Sustaining airfoils

Patent

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Details

244130, 277651, 277652, 277644, B64C 358, B64C 138, F16J 1500

Patent

active

059134941

ABSTRACT:
A blade seal (20) for an aircraft has a mounting structure (22). A composite blade (26) is attached to the mounting structure (22). The composite blade (26) has a plurality of holes (28). An elastomer substance (30) is used to fill the plurality of holes (28).

REFERENCES:
patent: 4471925 (1984-09-01), Kunz
patent: 5222699 (1993-06-01), Albach et al.
patent: 5794893 (1998-08-01), Diller et al.
patent: 5839698 (1998-11-01), Moppert

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